GB0302116D0 - A rotor - Google Patents
A rotorInfo
- Publication number
- GB0302116D0 GB0302116D0 GBGB0302116.9A GB0302116A GB0302116D0 GB 0302116 D0 GB0302116 D0 GB 0302116D0 GB 0302116 A GB0302116 A GB 0302116A GB 0302116 D0 GB0302116 D0 GB 0302116D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0302116.9A GB0302116D0 (en) | 2003-01-30 | 2003-01-30 | A rotor |
US10/747,585 US7056094B2 (en) | 2003-01-30 | 2003-12-30 | Rotor and a retaining plate for the same |
EP04250077A EP1443179B1 (fr) | 2003-01-30 | 2004-01-09 | Un rotor comportant des plaques de rétention |
DE602004019715T DE602004019715D1 (de) | 2003-01-30 | 2004-01-09 | Ein Rotor mit Schaufelhalteplatten |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0302116.9A GB0302116D0 (en) | 2003-01-30 | 2003-01-30 | A rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
GB0302116D0 true GB0302116D0 (en) | 2003-03-05 |
Family
ID=9952093
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB0302116.9A Ceased GB0302116D0 (en) | 2003-01-30 | 2003-01-30 | A rotor |
Country Status (4)
Country | Link |
---|---|
US (1) | US7056094B2 (fr) |
EP (1) | EP1443179B1 (fr) |
DE (1) | DE602004019715D1 (fr) |
GB (1) | GB0302116D0 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2890105A1 (fr) * | 2005-08-31 | 2007-03-02 | Snecma | Dispositif d'immobilisation d'un anneau de retention axiale d'une aube, disque de rotor et anneau de retention associes et rotor et motor d'aeronef les comportant |
FR2890104A1 (fr) * | 2005-08-31 | 2007-03-02 | Snecma | Dispositif d'immobilisation d'un anneau de retention axiale d'une aube, disque de rotor et anneau de retention associes et rotor et moteur d'aeronef les comportant |
GB0521242D0 (en) * | 2005-10-19 | 2005-11-23 | Rolls Royce Plc | A blade mounting |
FR2951224B1 (fr) * | 2009-10-13 | 2011-12-09 | Turbomeca | Roue de turbine equipee d'un jonc de retenue axiale verrouillant des pales par rapport a un disque |
FR3011032B1 (fr) * | 2013-09-25 | 2017-12-29 | Snecma | Ensemble rotatif pour turbomachine |
US10895160B1 (en) * | 2017-04-07 | 2021-01-19 | Glenn B. Sinclair | Stress relief via unblended edge radii in blade attachments in gas turbines |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB782181A (en) | 1954-09-27 | 1957-09-04 | Lloyd Calvin Secord | Rotor blade locking means |
US3023998A (en) * | 1959-03-13 | 1962-03-06 | Jr Walter H Sanderson | Rotor blade retaining device |
GB906476A (en) * | 1960-10-11 | 1962-09-19 | Fairweather Harold G C | Improvements in rotor assemblies for turbines, compressors and the like |
US3656865A (en) * | 1970-07-21 | 1972-04-18 | Gen Motors Corp | Rotor blade retainer |
US4566857A (en) * | 1980-12-19 | 1986-01-28 | United Technologies Corporation | Locking of rotor blades on a rotor disk |
FR2603333B1 (fr) * | 1986-09-03 | 1990-07-20 | Snecma | Rotor de turbomachine comportant un moyen de verrouillage axial et d'etancheite d'aubes montees dans des brochages axiaux du disque et procede de montage |
GB9517369D0 (en) | 1995-08-24 | 1995-10-25 | Rolls Royce Plc | Bladed rotor |
GB2313162B (en) * | 1996-05-17 | 2000-02-16 | Rolls Royce Plc | Bladed rotor |
US6234756B1 (en) * | 1998-10-26 | 2001-05-22 | Allison Advanced Development Company | Segmented ring blade retainer |
DE19960896A1 (de) * | 1999-12-17 | 2001-06-28 | Rolls Royce Deutschland | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
US6439851B1 (en) * | 2000-12-21 | 2002-08-27 | United Technologies Corporation | Reduced stress rotor blade and disk assembly |
-
2003
- 2003-01-30 GB GBGB0302116.9A patent/GB0302116D0/en not_active Ceased
- 2003-12-30 US US10/747,585 patent/US7056094B2/en not_active Expired - Fee Related
-
2004
- 2004-01-09 DE DE602004019715T patent/DE602004019715D1/de not_active Expired - Lifetime
- 2004-01-09 EP EP04250077A patent/EP1443179B1/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1443179A2 (fr) | 2004-08-04 |
US20040151591A1 (en) | 2004-08-05 |
US7056094B2 (en) | 2006-06-06 |
EP1443179B1 (fr) | 2009-03-04 |
EP1443179A3 (fr) | 2006-12-27 |
DE602004019715D1 (de) | 2009-04-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2403073B (en) | A stator core | |
GB0205584D0 (en) | Rotor | |
GB0320449D0 (en) | A rotor and a stator | |
GB0401663D0 (en) | A stator vane arrangement | |
GB0311159D0 (en) | A rotor blade arrangement | |
GB0526180D0 (en) | N/a | |
GB2406223B (en) | A rotor assembly | |
EP1536138A4 (fr) | Machine a rotor | |
EP1625160A4 (fr) | Bioelastomere | |
GB2397327B (en) | A screwpile | |
GB0606229D0 (en) | A golf-tee assembly | |
GB0302116D0 (en) | A rotor | |
GB2403269B (en) | A Pump | |
GB0202571D0 (en) | Rotor | |
GB0318033D0 (en) | A turbine | |
GB0303341D0 (en) | Rotor | |
GB0526009D0 (en) | N/a | |
GB0328266D0 (en) | A turbine | |
GB0302153D0 (en) | A rotor assembly | |
AU155263S (en) | A stator | |
GB2401999B (en) | A lead | |
TW584357U (en) | A dial-switch | |
GB0400753D0 (en) | A stator vane arrangement | |
AU156725S (en) | A rotor plate | |
AU152742S (en) | A photopuzzle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |